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KLH 3s 70 TL

KLH 3s 70 TL is a cross-laminated solid wood panel from KLH Massivholz GmbH, also known as KLH® - CLT. The panel has 3 layers and has a total thickness of 70mm. As a TL element, it is usually used as a ceiling and roof panel in solid timber construction. The crosswise arrangement of the longitudinal and transverse lamellas minimizes the swelling and shrinkage of the wood in the panel plane. At the same time, this increases the static load-bearing capacity and dimensional stability in the panel plane. Depending on the thickness and the presence of cladding, fire protection requirements of 30, 60, 90 and 120 minutes are met.

Graphical representation

KLH 3s 70 TL

KLH 3s 70 TL is a cross-laminated solid wood panel from KLH Massivholz GmbH, also known as KLH® - CLT. The panel has 3 layers and has a total thickness of 70mm. As a TL element, it is usually used as a ceiling and roof panel in solid timber construction. The crosswise arrangement of the longitudinal and transverse lamellas minimizes the swelling and shrinkage of the wood in the panel plane. At the same time, this increases the static load-bearing capacity and dimensional stability in the panel plane. Depending on the thickness and the presence of cladding, fire protection requirements of 30, 60, 90 and 120 minutes are met.

Stiffness and cross section properties for EDP-based analysis

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Stiffness Properties for the modelling of KLH-Elements as shear-flexible plate structure by means of FEM
Descriptionb = 1mUnit
XY
1
EJ
Bending stiffnessEJ31627kNm2/m
EJ - Bending stiffness [kNm2/m]
Bending stiffness
2
GJ
Torsional stiffnessGJ10.7kNm2/m
GJ - Torsional stiffness [kNm2/m]
Torsional stiffness
3
GA
Shear stiffnessGA4,45017,200kN/m
GA - Shear stiffness [kN/m]
Shear stiffness
4
EA
Extensional stiffnessEA480,000360,000kN/m
EA - Extensional stiffness [kN/m]
Extensional stiffness
5
GA2
In-plane shear stiffnessGA222,000kN/m
GA2 - In-plane shear stiffness [kN/m]
In-plane shear stiffness
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Stiffness Properties for the modelling of KLH-Elements as orthotropic plate by means of FEM
Descriptionb = 1mUnit
XY
1
tred
Reduced plate depthtred6830mm
tred - Reduced plate depth [mm]
Reduced plate depth
2
Gmean
G-Modulus for plate action1, 2Gmean78N/mm2
Gmean - G-Modulus for plate action1, 2 [N/mm2]
G-Modulus for plate action1, 2
3
Emean
E-Modulus (MOE) for plate actionEmean12,000N/mm2
Emean - E-Modulus (MOE) for plate action [N/mm2]
E-Modulus (MOE) for plate action
4
tred
Reduced membrane depthtred4030mm
tred - Reduced membrane depth [mm]
Reduced membrane depth
5
Gmean
G-Modulus for membrane action1, 3Gmean660N/mm2
Gmean - G-Modulus for membrane action1, 3 [N/mm2]
G-Modulus for membrane action1, 3
6
Emean
E-Modulus (MOE) for membrane actionEmean12,000N/mm2
Emean - E-Modulus (MOE) for membrane action [N/mm2]
E-Modulus (MOE) for membrane action
1) The shear modulus applies to the equivalent rectangular cross section and has been adapted accordingly (i.e. increased by a factor of 6/5), since the current FE programs generally do not allow any further specifications.
2) The shear modulus for the plate action specified here represents the less favourable value for the X and Y directions.
3) The shear modulus for the membrane action specified here represents the less favourable value for the X and Y directions.
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Stiffness Properties for the modelling of KLH-Elements as grillage using lattice frame software (shear-flexible)
Descriptionb = 1mUnit
XY
1
bred
Equivalent beam widthbred9211,000mm
bred - Equivalent beam width [mm]
Equivalent beam width
2
h
Beam depthh7030mm
h - Beam depth [mm]
Beam depth
3
Gmean
G-Modulus for plate action1, 2Gmean83688N/mm2
Gmean - G-Modulus for plate action1, 2 [N/mm2]
G-Modulus for plate action1, 2
4
Emean
E-Modulus (MOE) for plate actionEmean12,000N/mm2
Emean - E-Modulus (MOE) for plate action [N/mm2]
E-Modulus (MOE) for plate action
5
bred
Equivalent beam widthbred4030mm
bred - Equivalent beam width [mm]
Equivalent beam width
6
Gmean
G-Modulus for membrane action1, 3Gmean660880N/mm2
Gmean - G-Modulus for membrane action1, 3 [N/mm2]
G-Modulus for membrane action1, 3
7
Emean
E-Modulus (MOE) for membrane actionEmean12,000N/mm2
Emean - E-Modulus (MOE) for membrane action [N/mm2]
E-Modulus (MOE) for membrane action

Cross section properties for manual calculation

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Cross-section values
Descriptionb = 1mUnit
XY
1
Jnet,t
Net moment of inertia (tension side)Jnet,t2,633225cm4
Jnet,t - Net moment of inertia (tension side) [cm4]
Net moment of inertia (tension side)
2
Jnet,c
Net moment of inertia (compression side)Jnet,c2,633225cm4
Jnet,c - Net moment of inertia (compression side) [cm4]
Net moment of inertia (compression side)
3
Anet
Net cross-sectional areaAnet400300cm2
Anet - Net cross-sectional area [cm2]
Net cross-sectional area
4
Aeff
Effective cross-sectional areaAeff700300cm2
Aeff - Effective cross-sectional area [cm2]
Effective cross-sectional area
5
inet
Net radius of gyrationinet269mm
inet - Net radius of gyration [mm]
Net radius of gyration
6
es,Ra1
Distance between center of gravity and edge 1es,Ra13515mm
es,Ra1 - Distance between center of gravity and edge 1 [mm]
Distance between center of gravity and edge 1
7
es,Ra2
Distance between center of gravity and edge 2es,Ra23515mm
es,Ra2 - Distance between center of gravity and edge 2 [mm]
Distance between center of gravity and edge 2
8
Wnet,Ra1
Section Modulus for edge 1Wnet,Ra1752150cm3
Wnet,Ra1 - Section Modulus for edge 1 [cm3]
Section Modulus for edge 1
9
Wnet,Ra2
Section Modulus for edge 2Wnet,Ra2752150cm3
Wnet,Ra2 - Section Modulus for edge 2 [cm3]
Section Modulus for edge 2

Membrane actions (Tab. A)

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Characteristic load-carrying capacity for In-plane actions
Descriptionb = 1mUnit
XY
1
Nt,0,Rk
Tensile force – Constant distributionNt,0,Rk660450kN
Nt,0,Rk - Tensile force – Constant distribution [kN]
Tensile force – Constant distribution
2
Nt,0,m,Rk
Tensile force – Variable distributionNt,0,m,Rk960650kN
Nt,0,m,Rk - Tensile force – Variable distribution [kN]
Tensile force – Variable distribution
3
Nc,0,Rk
Compressive force – Without column stability problemNc,0,Rk960650kN
Nc,0,Rk - Compressive force – Without column stability problem [kN]
Compressive force – Without column stability problem
4
Nc,loc,Rk
Compressive force – Narrow side – Local load introductionNc,loc,Rk1,4401,080kN
Nc,loc,Rk - Compressive force – Narrow side – Local load introduction [kN]
Compressive force – Narrow side – Local load introduction
5
Nc,90,Rk
Compressive force – Narrow side – Compression perpendicularNc,90,Rk416178kN
Nc,90,Rk - Compressive force – Narrow side – Compression perpendicular [kN]
Compressive force – Narrow side – Compression perpendicular
6
Nc,2.73,Rk
Compressive force – Column stability – Buckling lenght: 2.73 mNc,2.73,Rk29829kN
Nc,2.73,Rk - Compressive force – Column stability – Buckling lenght: 2.73 m [kN]
Compressive force – Column stability – Buckling lenght: 2.73 m
7
Nc,2.95,Rk
Compressive force – Column stability – Buckling lenght: 2.95 mNc,2.95,Rk26025kN
Nc,2.95,Rk - Compressive force – Column stability – Buckling lenght: 2.95 m [kN]
Compressive force – Column stability – Buckling lenght: 2.95 m
8
Nc,3.50,Rk
Compressive force – Column stability – Buckling lenght: 3.50 mNc,3.50,Rk19118kN
Nc,3.50,Rk - Compressive force – Column stability – Buckling lenght: 3.50 m [kN]
Compressive force – Column stability – Buckling lenght: 3.50 m
9
Nc,5.00,Rk
Compressive force – Column stability – Buckling lenght: 5.00 mNc,5.00,Rk98-kN
Nc,5.00,Rk - Compressive force – Column stability – Buckling lenght: 5.00 m [kN]
Compressive force – Column stability – Buckling lenght: 5.00 m
10
Nxy,KF,Rk
In-plane shear force – General actionNxy,KF,Rk180kN
Nxy,KF,Rk - In-plane shear force – General action [kN]
In-plane shear force – General action
11
VTR,Rk
In-plane shear force – Beam-like elements (H = 1 m)VTR,Rk219149kN
VTR,Rk - In-plane shear force – Beam-like elements (H = 1 m) [kN]
In-plane shear force – Beam-like elements (H = 1 m)

Plate actions (Tab. B)

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Characteristic load-carrying capacity for out-of-plane actions
Descriptionb = 1mUnit
XY
1
Mc,Rk
Bending moment – Compression edgeMc,Rk1,806360kNcm
Mc,Rk - Bending moment – Compression edge [kNcm]
Bending moment – Compression edge
2
Mt,Rk
Bending moment – Tension edgeMt,Rk1,806360kNcm
Mt,Rk - Bending moment – Tension edge [kNcm]
Bending moment – Tension edge
3
VRk
Shear forceVRk63.254kN
VRk - Shear force [kN]
Shear force

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